IP Library Granted Patent US 9,494,080
Granted Patent B2
US 9,494,080 · App. 14/246,760 · Granted Nov 15, 2016

Fuel pumping unit

Inventors: David Nicholas Neate (Warwickshire, GB); Jonathan Masters (Birmingham, GB)
Assignee: ROLLS-ROYCE CONTROLS AND DATA SERVICES LIMITED
F02C7/236F02C7/14F02C7/16F04B23/12F04C2/18F04C11/005F04C15/0096F04C2210/1044Y10T137/6579
View Patent ↗
Loading inventors, assignments & file history…
Monitor This Case
Get email alerts when status or documents change.
Order Certified Copies
Most orders are placed with the USPTO same day — all within 24 business hours.
Order via The Patent Place →
Pre-filled with this patent's details
Quick Facts
Patent No.
US 9,494,080
App. No.
14/246,760
Granted
Nov 15, 2016
Kind
B2
Abstract

A fuel pumping unit has a low pressure pump, a high pressure pump, and a drive input which drives the low and high pressure pumps. The low pressure pump supplies, in use, fuel at a boosted pressure to the high pressure pump. The fuel pumping unit further has a low pressure housing containing the low pressure pump, and a high pressure housing containing the high pressure pump. The housings are joined together at a housing interface. The drive input is contained in one of the housings, whereby drive from the drive input is transferred across the interface to the pump in the other housing. The housing interface includes a gap which interposes between the high pressure pump and the low pressure pump. A layer of substantially stagnant fuel is trapped, in use, in the gap to reduce heat transfer from the high pressure pump to the low pressure pump.

Claims (17)

1. A fuel pumping unit having a low pressure pump, a high pressure pump, and a drive input which drives the low and high pressure pumps, the low pressure pump supplying, in use, fuel at a boosted pressure to the high pressure pump;

wherein the fuel pumping unit further has a low pressure housing containing the low pressure pump, and a high pressure housing containing the high pressure pump, the housings being joined together at a housing interface, and the drive input being contained in one of the housings, whereby drive from the drive input is transferred across the interface to the pump in the other housing;

wherein the housing interface includes a gap which interposes between the high pressure pump and the low pressure pump, a layer of substantially stagnant fuel being trapped, in use, in the gap to reduce heat transfer from the high pressure pump to the low pressure pump; and

wherein fuel leaks into the gap from the high pressure housing to form the layer of stagnant fuel.

2. A fuel pumping unit according to claim 1 , wherein the gap in which the layer of stagnant fuel is trapped extends over at least 30% of the area of the housing interface.

3. A fuel pumping unit according to claim 1 , wherein the gap is at most 1.5 mm wide.

4. A fuel pumping unit according to claim 1 , wherein the gap is at least 0.5 mm wide.

5. A fuel pumping unit according to claim 1 which further has a spacer insert located at the housing interface, the gap being formed between a surface of the spacer insert and a surface of the low or high pressure housing.

6. A fuel pumping unit according to claim 5 , wherein the spacer insert is formed from a material having a thermal conductivity of at least 100 Wm −1 K −1 .

7. A fuel pumping unit according to claim 5 , wherein the spacer insert is formed from aluminium alloy.

8. A fuel pumping unit according to claim 5 , wherein the spacer insert is located in a recess formed in the low or high pressure housing.

9. A fuel pumping unit according to claim 5 , wherein the spacer insert includes an aperture through which drive from the drive input is transferred across the interface to the pump in the other housing.

10. A fuel pumping unit according to claim 1 which further has one or more air gaps at the housing interface.

11. A fuel pumping unit according to claim 1 wherein the fuel pumping unit is suitable for pumping fuel for an aero-engine.

12. A fuel pumping system having the fuel pumping unit according to claim 1 and a fuel/oil heat exchanger which uses the fuel to cool lubrication oil, a fuel inlet of the fuel/oil heat exchanger receiving fuel from the low pressure pump and a fuel outlet of the fuel/oil heat exchanger supplying fuel to the high pressure pump.

13. An aero-engine having the fuel pumping unit according to claim 1 .

14. An aero-engine having the fuel pumping system according to claim 12 .

Assignments (2)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Aug 7, 2017
From: ROLLS-ROYCE CONTROLS AND DATA SERVICES LIMITED
To: ROLLS-ROYCE PLC
Reel/Frame 043219/0929 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Apr 7, 2014
From: NEATE, DAVID NICHOLAS; MASTERS, JONATHAN
To: ROLLS-ROYCE CONTROLS AND DATA SERVICES LIMITED
Reel/Frame 032622/0086 →
Priority Claims (1)
GB 1309049.3 · May 20, 2013 · national
Continuity (1)
Related Publication 20140338759A1 · Nov 20, 2014